陈志英,李建福,周平,刘勇.航空发动机直通型篦齿径向变形稳健性优化[J].航空发动机,2018,44(1):1-6
航空发动机直通型篦齿径向变形稳健性优化
Robust Optimization for Straight-through Labyrinth Seal Radial Deformation of Aeroengine
  
DOI:
中文关键词:  直通型篦齿  径向变形  最小二乘支持向量机  稳健性  概率分位数区间
英文关键词:straight-through labyrinth seal  radial deformation  LS-SVM  robust  probability of quantile interval
基金项目:国家自然科学基金(51275024)资助
作者单位E-mail
陈志英,李建福,周平,刘勇 北京航空航天大学能源与动力工程学院北京100191 chenzhiying@buaa.edu.cn 
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中文摘要:
      为了降低参数不确定性对发动机直通型篦齿径向变形的影响,提出了一种基于最小二乘支持向量机(LS-SVM)和概率分 位数区间模型的稳健性优化方法。通过LS-SVM 建立参数与篦齿径向变形的响应面近似模型,考虑到参数不确定性分布类型的差异 性,采用概率分位数区间方法建立稳健性优化模型,对篦齿结构径向变形进行了稳健性优化设计。结果表明:优化后的篦齿结构径 向变形概率分位数区间比优化前减少6%,参数灵敏度分析结果也验证了该优化方法的有效性
英文摘要:
      In order to reduce the influence of parameter uncertainty on the radial deformation of straight-through labyrinth seal of aeroengine, a robust optimization method was proposed based on Least Squares Support Vector Machine 渊LS-SVM冤and probabilistic quantile interval model. The LS-SVM was used to establish the response surface approximation model between parameters and labyrinth seal radial deformation. Considering the diversity of uncertainty distribution types of parameters, the probabilistic quantile interval method was adopted to establish robust optimization model. The method was used to optimize the radial deformation of labyrinth seal. The results show that the probabilistic quantile interval of radial deformation on labyrinth seal is reduced by 6%compared with that before optimization. The effectiveness of the method is also verified by the results of parameter sensitivity analysis
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